Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
39 in
|
| gptkbp:firstFlight |
1946
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
147 in
|
| gptkbp:manufacturer |
gptkb:Allison_Engine_Company
|
| gptkbp:numberOfStages |
2
11 |
| gptkbp:status |
retired
|
| gptkbp:thrust |
5,200 lbf
|
| gptkbp:usedInAircraft |
gptkb:Lockheed_F-94_Starfire
gptkb:Republic_F-84_Thunderjet North American F-86 Sabre (early prototypes) |
| gptkbp:weight |
2,455 lb
|
| gptkbp:bfsParent |
gptkb:F-84G
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Allison J35-A-29 turbojet
|